Methods and systems for efficient installation of cables in watercraft

ABSTRACT

The present application is directed towards systems and methods for efficient installation of optical and electrical cable in watercraft. A manufacturer may terminate one end of a cable in a location removed from the watercraft, allowing use of automated cable termination machines for efficiency and consistency of terminations. The single-terminated cable may then be brought to the watercraft and installed by pulling or routing the unterminated end through ductwork and pipes, watertight bulkhead throughways, and cable trays and ladders as necessary, prior to termination. Accordingly, more difficult and expensive on-site labor is reduced, and reliability is greatly increased. Furthermore, many cable tests that require termination but cannot be executed post-installation can be performed prior to installation, to ensure that at least the first termination, performed off-site, is error-free, reducing later troubleshooting and further increasing installation efficiency.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of U.S. patent application Ser. No.13/560,543, filed on Jul. 27, 2012, which claims the benefit of U.S.patent application Ser. No. 12/869,916, filed Aug. 27, 2010, now U.S.Pat. No. 8,254,738. Each of the aforementioned applications and issuedpatents is hereby incorporated by reference in its entirety.

FIELD OF THE INVENTION

The present application generally relates to cable installation. Inparticular, the present application relates to systems and methods forefficient installation of optical and electrical cable in watercraft.

BACKGROUND OF THE INVENTION

Vehicles, including automobiles, trucks, watercraft, and aircraft, haveincluded electrical cabling for over a century. Electrical cabling hasbeen in use on watercraft in particular since the early 1880s, whenelectric lights were first installed on the H.M.S. Inflexible. However,installation of these cables can be tedious and inefficient, due to therequirements of space, weight, and the amount of cabling required. Forexample, a modern airplane or ship may have more than a hundred miles ofelectrical wiring.

In the past, wiring has been installed in these vehicles using similarmethods to those used in building construction: during the initialframing, while walls are still open, wires may be manually passed fromone section to another and cut to length. After the walls are finished,the wires may be terminated in outlets and switches or other connectors.Accordingly, electricians are required to perform part of their work atone time, and part at another time, complicating project management andincreasing expense. Unlike building construction, however, many landvehicles and aircraft are manufactured in mass assembly lines. Therequirement of pausing assembly at a first stage to install electricalwiring and then returning at another stage to terminate wires reducesthe efficiency gained in automation.

To reduce this inefficiency, manufacturers have taken advantage of theconsistency of manufactured parts generated by assembly lines. Becausethe wires in every car of a specific model will be the same length andfollow the same routing path, rather than pulling wires individually inthe finished vehicle and cutting them to length, electricians can useworktables customized for the installation. For example, shown in FIG.1A is a diagram of an embodiment of a wire harness 100 assembled on awireboard 102. The wireboard may be plywood or other materials, and mayinclude pins or nails 104 placed along a path. Wires 106 may be routedalong the paths defined by these pins and cut to lengths specified onthe wireboard 102. Connectors 108 may be installed on the wireboard, andthe wires may be tied or bundled together to form the harness. Referringnow to FIG. 1B, the preassembled wire harness 100 may be removed fromthe wireboard and installed into a vehicle, confident in the knowledgethat each wire will be the proper length for the various bends and turnsit needs to take to reach instrument panels, switches, or othercomponents.

The same technique may be used in the construction of a wire harness foran aircraft. Referring now to FIG. 2A, shown is a diagram of anembodiment of an airplane wire harness 200 assembled on a wireboard 202.The wireboard 202 may be a many pieces of plywood or other materialsplaced together to form a full-size outline of the aircraft. In someinstances, due to the size involved, wireboard 202 may not physicallyexist, but rather comprise a large open space, such as the floor of anairplane hangar or manufacturing plant and be painted or marked with anoutline of the aircraft 203 or the locations of various componentswithin the finished aircraft. In other embodiments, as shown in FIG. 1A,wires may be looped back on themselves to achieve the necessary lengthwithout requiring a full-size mockup. Similar to the creation of a wireharness shown in FIG. 1A, in FIG. 1B, wires 206 may be routed along pins204 to final locations, cut to length, and terminated. The wires maythen be tied or bundled to form a finished wire harness 200. Referringnow to FIG. 2B, the preassembled wire harness 200 may be installed intopremanufactured sections of the aircraft 210. Because the wire harnessmay be assembled separately from the vehicle, electricians can preparemultiple harnesses concurrently, increasing efficiency.

As shown in FIG. 2B, aircraft are manufactured in sections, which maythen be joined together, simplifying installation. A wire harnessstretching the full length of the aircraft can be run through openingsbetween each section, and as the sections are brought together, may beattached to mounting points or connected to terminations such asengines, control surfaces, instrument panels, and other features.Vehicles are similarly constructed in sections that are joined together,such as doors bolted on to the main body. Accordingly, a wire harnessmay be fed through openings in the body and doors prior to attachment,and the openings may be of sufficient size to accommodate the largeconnectors required for multi-conductor cables.

Installation of cables into watercraft poses significant additionalproblems, however. Shown in FIG. 3 is a cutaway diagram of an embodimentof a watercraft 300. Unlike manufacture of aircraft and automobiles,watercraft are frequently constructed by laying watertight bulkheads 304along a keel and affixing the hull 302 at one time. Because of thewatertight sections, pre-terminated wire harnesses may not be able to bepulled through bulkhead openings.

Furthermore, while a large assembly line may output thousands of carsper day with identical wire run lengths, ships are frequently customdesigned or customized from a base design. Accordingly, even two shipsbuilt in succession by the same manufacturer may have very differentwiring requirements. In the modern industrial shipbuilding techniqueknown as block construction, sections of a large watercraft are builtseparately before being bolted and welded together. Although similar tothe sectioned construction of aircraft shown in FIG. 2B, thecustomization of watercraft means that prebuilt wire harnesses cannot beused even in these manufacturing techniques, because of imprecisecalculations of wire run lengths. One answer would be to simply makeevery wire longer than necessary and leave the excess in loops at oneend. However, this adds significant weight and takes up large amounts ofroom, particularly with the hundreds of miles of wiring in modernwatercraft. Furthermore, because connectors used in watercraft arefrequently large, particularly for military-grade or MIL-SPECinstallations required on naval vessels or when a cable includesmultiple conductors to be terminated in a multi-pin connector, theconnectors may be too large to be preinstalled and pulled throughwatertight cable throughways, ductwork, and other pass-throughs inwatertight bulkheads. Accordingly, cables are still installed inwatercraft today in the same inefficient pull-cut-terminate method usedover one hundred years ago.

BRIEF SUMMARY OF THE INVENTION

The present application is directed towards systems and methods forefficient installation of optical and electrical cable in watercraft. Amanufacturer may terminate one end of a cable in a location removed fromthe watercraft, allowing use of automated cable termination machines forefficiency and consistency of terminations. The single-terminated cablemay then be brought to the watercraft and installed by pulling orrouting the unterminated end through ductwork and pipes, watertightbulkhead throughways, and cable trays and ladders as necessary, prior totermination. Accordingly, more difficult and expensive on-site labor isreduced, and reliability is greatly increased. Furthermore, many cabletests that require termination but cannot be executed post-installationcan be performed prior to installation, to ensure that at least thefirst termination, performed off-site, is error-free, reducing latertroubleshooting and further increasing installation efficiency.

In one aspect, the present invention features a method for efficientinstallation of cable in a watercraft. The method includes terminating,at a location different from a watercraft, a first end of a cable to beinstalled. The method also includes installing the cable on thewatercraft. The method further includes terminating a second end of theinstalled cable.

In some embodiments, the method includes the location different from thewatercraft comprising a cable manufactory. In many embodiments, themethod includes the cable comprising a multi-conductor cable. In someembodiments, the method includes the cable comprising an optical fibercable. In other embodiments, the method includes the cable comprising anelectrical cable.

In one embodiment, the method includes installing a connector on thecable. In a further embodiment, the method includes the connectormeeting a military standard (MIL-SPEC). In another further embodiment,the method includes testing performance of the installed connector atthe location different from the watercraft. In a still furtherembodiment in which the cable comprises a multi-conductor cable, themethod includes performing a high potential (referred to variously as a“hi-potential”, “hi-voltage”, “hi-pot” or “hipot”) test between aplurality of conductors of the multi-conductor cable. In another stillfurther embodiment, the method includes terminating the second end ofthe installed cable at the location different from the watercraft,testing performance of the installed connector with the terminatedsecond end, and removing the terminated second end of the installedcable prior to installing the cable on the watercraft.

In some embodiments, the method includes routing the cable through amulti-cable throughway in a watertight bulkhead. In other embodiments,the method includes routing the cable through a plurality ofcompartments.

In one embodiment, the method includes determining a first length of afirst cable run on the watercraft and a second length of a second cablerun on the watercraft, cutting a cable to third length of at least thefirst length plus the second length, terminating the first end of thecable, terminating the opposite end of the cable, and cutting the cableat a position at least the first length from the first terminated end.In a further embodiment, the method includes testing the performance ofthe cable prior to cutting the cable at the position at least the firstlength from the first terminated end. In another further embodiment, themethod includes cutting the cable to create a second cable of length ofat least the first length with a single terminated end and a third cableof length of at least the second length with a single terminated end,installing the second cable and the third cable on the watercraft, andterminating an unterminated end of the second cable and terminating anunterminated end of the third cable.

In another aspect, the present invention features a method for efficientmanufacture of cable for a watercraft. The method includes determining afirst length of a first cable run on the watercraft and a second lengthof a second cable run on a watercraft. The method also includes cuttinga cable to a third length of at least the first length plus the secondlength. The method further includes terminating the first end of thecable. The method also includes terminating the second end of the cable.The method also includes cutting the cable at a position at least thefirst length from the first terminated end.

In some embodiments, the method includes testing the performance of theterminated first end and terminated second end of the cable prior tocutting the first cable. In one embodiment, the cable comprises anoptical fiber cable. In another embodiment, the cable comprises anelectrical cable. In another aspect, the present invention features asingle-terminated cable made by the method for efficient manufacture ofcable for a watercraft.

The details of various embodiments of the invention are set forth in theaccompanying drawings and the description below.

BRIEF DESCRIPTION OF THE FIGURES

The foregoing and other objects, aspects, features, and advantages ofthe invention will become more apparent and better understood byreferring to the following description taken in conjunction with theaccompanying drawings, in which:

FIG. 1A is a diagram of an embodiment of a wire harness assembled on awireboard;

FIG. 1B is a diagram of an embodiment of an assembled wire harness;

FIG. 2A is a diagram of an embodiment of an airplane wire harnessassembled on a wireboard;

FIG. 2B is an exploded view of an embodiment of installation of anairplane wire harness into an airplane;

FIG. 3 is a cutaway diagram of an embodiment of a watercraft;

FIG. 4 is a flow chart of an embodiment of a method of efficient cablemanufacturing, testing, and installation into a watercraft; and

FIGS. 5A and 5B are a flow chart of another embodiment of a method ofefficient cable manufacturing, testing, and installation into awatercraft.

The features and advantages of the present invention will become moreapparent from the detailed description set forth below when taken inconjunction with the drawings, in which like reference charactersidentify corresponding elements throughout. In the drawings, likereference numbers generally indicate identical, functionally similar,and/or structurally similar elements.

DETAILED DESCRIPTION OF THE INVENTION

For purposes of reading the description of the various embodimentsbelow, the following descriptions of the sections of the specificationand their respective contents may be helpful:

Section A describes methods for efficient cable manufacture andinstallation into watercraft;

Section B describes systems and methods for termination and testing ofelectrical cables using embodiments of the efficient manufacture andinstallation methods described herein; and

Section C describes systems and methods for termination and testing ofoptical fiber cables using embodiments of the efficient manufacture andinstallation methods described herein.

A. Efficient Cable Manufacture and Installation into Watercraft

As discussed above, in many instances of installing cables onwatercraft, due to customization, exact lengths of cable runs may not beknown in advance. Furthermore, even when exact runs may be calculated ormeasured from plans, in practice, cables may wrap around other cableswhen pulled or take larger radius paths through bends, reducing theeffective length that can be pulled. Accordingly, if an installer cuts acable to a precisely calculated length for a run, once installed, thecable may be short by a foot or more. Due to the exacting standards ofmilitary-standard compliant (MIL-SPEC) installations, in some instances,cables may not be spliced to add additional length. Instead, the cablemust be removed and replaced with a longer cable, increasing expense andinstallation time.

Additionally, due to space considerations, it may be difficult toterminate cables within the watercraft. Some cables may end in crampedspaces, behind unmovable equipment racks, or in locations of limitedaccessibility such as in radio masts or behind engines. Because manyconnectors may be large, particularly rugged MIL-SPEC connectors orconnectors for multi-conductor cables, in-place termination may betough, time-consuming and error-prone.

Accordingly, in many embodiments, it may be preferable to terminate oneend of a cable in a location removed from the watercraft. For example, amanufacturer may terminate one end of a cable at a factory, allowing useof automated cable termination machines for efficiency and consistencyof terminations. The single-terminated cable may then be brought to thewatercraft and installed by pulling or routing the unterminated endthrough ductwork and pipes, watertight bulkhead throughways, and cabletrays and ladders as necessary. The unterminated end may then beterminated. Due to the difficulty of in-place termination, theefficiency gained by terminating one end of the cable in an easieroff-site location is frequently greater than 50%, because fewerterminations will need to be re-done due to shorts or weak connections.Additionally, as discussed in more detail below, many cable tests may beperformed off-site that could not be performed after installation.Performing these tests may ensure that the first termination, performedoff-site, is error-free, reducing later troubleshooting and furtherincreasing installation efficiency.

In some embodiments, additional installation efficiency can be gained bystrategically selecting which end of a cable to terminate off-site. Forexample, in many embodiments, a cable may be run between two locations,one of which may a difficult or cramped place to access for terminationpurposes, such as behind immovable equipment, in small between-deckareas, on radio masts, or other areas that may be difficult for aninstaller to reach or comfortably work in during termination.Accordingly, by selecting these locations and pre-terminating the endsof cables to be installed in these locations in a more comfortable worklocation off-site, an installer can work more efficiently.

Similarly, in many embodiments, many cables may be run from a firstlocation, such as a control room, to locations all over the watercraft.Termination of cables frequently requires equipment to be set up,including soldering irons, work tables or clamps, bright lighting,magnifiers, or other tools. It may be preferable in these embodiments toreduce the need for installers to move these tools around thewatercraft. By strategically selecting and pre-terminating the ends ofthese cables that will be installed in the locations around thewatercraft, the installer will be able to remain in the first location,such as the control room, and terminate all of the unterminated ends ofthese cables without having to transport his or her tools around thewatercraft.

Referring now to FIG. 4, a flow chart of an embodiment of a method 400of efficient cable manufacturing, testing, and installation into awatercraft is shown. In brief overview, at step 402, an installer ormanufacturer may terminate a first end of a cable. At step 404, thecable may be installed in the watercraft. At step 406, the installer mayterminate the second end of the cable. In some embodiments utilizing anoff-site testing procedure, prior to step 404, the second end of thecable may be terminated at step 408. The cable terminations may betested at step 410. At step 412, the second termination may be removed.The cable may then be installed at step 404 and terminated at step 406as above.

Still referring to FIG. 4 and in more detail, at step 402, an installeror manufacturer may terminate a first end of a cable at a locationdifferent from a watercraft intended for installation of the cable. Insome embodiments, the location different from the watercraft maycomprise a cable manufactory or other manufacturing location. In otherembodiments, the location different from the watercraft may comprise atemporary or permanent termination installation area, such as awarehouse or other location. In some embodiments, the cable may be asingle-conductor cable, such as a grounding cable, while in otherembodiments, the cable may be a multi-conductor cable. Multi-conductorcables may include, without limitation, coaxial cables, untwisted ortwisted pair cables, multi-pair cables, serial or parallel data cablesincluding USB cables, Ethernet cables such as Cat-3, Cat-5, Cat-6 or anyother standard, balanced or unbalanced audio cables, composite orcomponent video cables, digital video cables including HDMI and DVIvideo cables, single or multi-mode optical fiber cables, or anycombination of electrical and/or optical fiber cables.

In some embodiments, terminating the first end of the cable may compriseinstalling a connector on the cable, discussed in more detail below inparts B and C, with reference to electrical and optical fiber cables,respectively. In many embodiments, the connector may meet a militarystandard, such as a MIL-SPEC connector. Once the first end of the cableis terminated, in some embodiments, the cable may be placed onto a spoolor reel for ease of storage, transportation, and unwinding duringinstallation. In many embodiments, the cable may be cut to a lengthgreater than the distance the cable is to run on the watercraft. Forexample, if a cable is to run 300′ from one compartment to another, thecable may be cut to a length greater than 300′, such as 330′. Thisprovides a 10% margin of error in measurement or for the cable to wraparound other cables during routing. Prior to terminating the second endof the cable, the cable may be cut to a final installation length.

At step 404, the cable may be installed in the watercraft. In someembodiments, the cable may be installed within a single compartment,while in other embodiments, the cable may be installed through aplurality of compartments. For example, in one such embodiment, thecable may be installed from an engine room to a wheelhouse or controlcenter. In many embodiments, installing the cable may comprise routingthe cable through a single-cable or multi-cable throughway (MCT), or awatertight cable pass-through in a watertight bulkhead. The cablethroughway may comprise a pipe, tube, hole, or other pass-through andmay include a sealing material, and installing the cable may compriseinstalling the cable through or with the sealing material. In otherembodiments, installing the cable may comprise routing or pulling thecable through ductwork or pipes or other pass-throughs between decks,which may be variously watertight or non-watertight. Installing thecable may also comprise routing the cable via cable trays or laddertrays or through retaining rings. In some embodiments, installing thecable may also comprise tying or securing the cable in bundles or tocable retainers.

In some embodiments, the cable may be installed starting from a firstlocation where the first terminated end of the cable will be connected.For example, in one such embodiment with a single-terminated cable to berun from an engine room to a wheelhouse with the terminated end to beconnected to equipment in the engine room, the unterminated end of thecable may be pulled or routed from the engine room to the wheelhouse. Inmany embodiments, particularly involving routing cable through pipes orducts, a wire snake may be first pushed through the pipe or duct. Thecable may be tied or otherwise attached to the snake, and the snake maybe pulled back through the pipe or duct to pull the cable. In otherembodiments, the snake may first pull a pull string through the pipe,and the cable may then be attached to the pull string and pulled throughthe pipe. In some embodiments, because excessive strain may damageconductors in a cable, strain gages may be attached to the cable duringpulling and monitored for overall strain.

Once the second end of the cable has been pulled to its final location,at step 406, the second end of the cable may be terminated. As discussedabove, terminating the cable may comprise installing a connector ontothe cable, discussed in more detail below.

As discussed above, by terminating the cable at a location removed fromthe watercraft, in many embodiments testing may be performed on thecable that could not be performed or as easily performed afterinstallation. For example, and discussed in more detail below, in atypical installation, an installed and terminated cable may be testedfor continuity along each conductor: a voltage may be applied to pin 1on one connector and measured on pin 1 of the other connector to checkfor breaks. The voltage may then be applied to pin 2 and measured on pin2; applied to pin 3 and measured on pin 3; and so on until continuity ofall conductors has been measured. In some embodiments, rather than asteady voltage, a signal or tone may be applied and detected on theother connector. While these tests ensure continuity, they don't detectshorts or breaks in insulation. For example, due to a break ininsulation within the cable or a short in one of the terminations, avoltage applied to pin 1 may also show up on pin 3. Normal continuitytests would fail to detect this condition, and testing between pins isnot ordinarily performed after installation on the watercraft due to thetime and expense involved: a multi-conductor cable with fifty conductorscould require 50^50 or more than 10^84 continuity tests, and a largewatercraft may have hundreds or thousands of such cables installed.

Furthermore, continuity tests performed after installation are usuallyat low-voltage, for safety reasons: at high voltage, a short circuitcould start a fire inside a between-deck duct, resulting in significantdamage. However, such low-voltage tests may not detect worn insulationthat may fail to insulate at higher voltages, short circuits that havehigh resistance due to oxidation, or broken insulation between twoconductors that are nonetheless separated by a slight gap.

Automated, high voltage or potential (hi-pot) tests may be efficientlyperformed in a location removed from the watercraft. In someembodiments, these tests may require terminating the second end of thecable at step 408. In many embodiments, terminating the second end ofthe cable may comprise installing a connector onto the cable, as at step402. At step 410, the cable and terminations may be tested. In someembodiments, testing may be performed manually, while in otherembodiments, automated testing may be performed. Testing methods arediscussed in more detail below.

At step 412, the second termination may be removed. In some embodiments,removing the second termination may comprise cutting the cable while inother embodiments, removing the second termination may comprise removingor desoldering components of the terminated connector. After removal ofthe termination, method 400 may proceed with steps 404 and 406.

Referring now to FIGS. 5A and 5B, shown is a flow chart of anotherembodiment of a method 500 of efficient cable manufacturing, testing,and installation into a watercraft. In brief overview, at step 502, afirst length may be determined for a first cable run on a watercraft. Atstep 504, a second length may be determined for a second cable run onthe watercraft. At step 506, a first cable may be cut to a third lengthof at least the first length plus the second length. At step 508, thefirst end of the first cable may be terminated. At step 510, the secondend of the first cable may be terminated. At step 512, the cableterminations and cable may be tested. At step 514, the first cable maybe cut into a second single-terminated cable of length of at least thefirst length, and a third single-terminated cable of length of at leastthe second length. At step 516, the second and third single-terminatedcables may be installed in the watercraft. At step 518, the cut end ofthe second cable may be terminated. At step 520, the cut end of thethird cable may be terminated.

In many embodiments, method 500 may provide increased efficiency byreducing the loss due to cutting the second terminated end in method400. Method 500 may also provide consistency in the use of telescopicgrounds to avoid electrical ground loops. Telescopic grounds are usedwith balanced wiring in which two conductors carry a balanced signal forincreased resistance to common-mode interference, such as balancedaudio, or RS-422 or 485 serial data. These conductors are frequentlysurrounded by a foil or braided wire Faraday shield for increasedresistance to electrostatic interference. The shield must be connectedto an electrical ground to provide shielding, but connecting the shieldto two grounds in different locations at different electrical potentialsmay result in an electrical current through the shield. This can be asource of audio hum or other noise, interfere with telemetry data, andcause other unwanted effects. One solution is to connect the shield atonly one end of a cable run, but this may create problems in ensuringconsistency, particularly with unsupervised installers in a watercraft.By using method 500 and connecting the shield to terminations at steps508 and 510, shield continuity and terminations may be fully tested atthe factory. On the watercraft, installers need not connect any shieldsat steps 518 and 520, reducing complexity and the amount of work to doin cramped spaces and reducing or even eliminated the chances of shieldsbeing left unconnected or being double-connected.

Still referring to FIGS. 5A and 5B and in more detail, at steps 502 and504, a first length of a first cable run on the watercraft and secondlength of a second cable run on the watercraft may be determined. Insome embodiments, determining the first length and the second length maycomprise measuring lengths on a scale plan or schematic. In otherembodiments, determining the first length or the second length maycomprise running a string, wire, or small cable along the cable run andmeasuring its length. In a similar embodiment, a string or wire can berun along the cable run, marked, and then used as a guide for cuttingcables to the proper length for the run, without needing to explicitlymeasure the length. In many embodiments, multiple cables will be runalong the same path, and accordingly, the first length and second lengthmay be equal. In a similar embodiment in which the first and cable runsare between the same compartments of the watercraft, the first lengthand the second length may be close, with a small amount ofintra-compartment length difference.

At step 506, in some embodiments, a first cable may be cut to a thirdlength of at least the first length plus the second length. In manyembodiments, to allow for a margin of error in measurement, routing, andterminating the first cable, the third length may be equal to the firstlength plus the second length, plus a safety margin. Such safety marginmay be a percentage, such as an additional ten percent length, or may bea predetermined amount, such as 10′, 20′, 30′, 50′, or more or less,depending on the overall length, the size of the connectors andlikelihood of needing to replace an improperly terminated connector, andany other factor. The cable may be a single or multi-conductor cable andmay comprise electrical conductors, optical fiber, or a combination ofelectrical conductors and optical fibers. Although referred to asfibers, because optical fibers conduct light, an optical fiber may bereferred to as a single conductor, and a bundle of optical fibers or amix of optical fibers and electrical conductors may be referred to as amulti-conductor cable herein. In many embodiments, the first cable maycomprise a cable type to be used for each of the first cable run and thesecond cable run.

At steps 508 and 510, the first end of the first cable and second end ofthe first cable may be terminated, respectively, using any of themethods discussed herein. In some embodiments, terminating the first endof the first cable and terminating the second end of the first cable maycomprise terminating the ends with the same connectors or with differentconnectors. For example, in one embodiment, the first end may beterminated with a male connector and the second end may be terminatedwith a female connector, while in other embodiments, the first end andsecond end may both be terminated with male connectors or femaleconnectors. In some embodiments, the first end and second end may beterminated with different types of connectors, such as a straight plugas opposed to an angled plug; a wall-mount receptacle as opposed to abox-mount or in-line receptacle; different keying positions; differentnumbers of pins; different positions of pins, such as a 15-pin three-rowsubminiature DE-15 commonly used for VGA, SVGA, or XGA, as opposed tothe 15-pin two-row subminiature DA-15 used for the X.21 standard or insome keyboard-video-mouse extenders.

At step 512, performance of the terminations and cable may be tested.Discussed in more detail below in sections B and C, various tests may beperformed on the electrical and optical conductors and connectors toensure continuity, lack of short-circuits, impedance, insulation andconnector resistance and other features.

At step 514, the first cable may be cut into a second cable of at leastthe first length and a third cable of at least the second length tocreate two single-terminated cables. As discussed above, in embodimentsin which the first cable is longer than the first length plus the secondlength to include a safety margin, the first cable may be cut such thatthe second cable is longer than the first length plus a safety marginand the third cable is longer than the second length plus a safetymargin. In some embodiments, the length of the first cable comprisingthe safety margin may be split evenly between the second cable and thirdcable, while in other embodiments, the first cable may be cut to createa greater safety margin in either the second or third cable. This may bedone, for example, where the final location of a piece of equipment in acompartment is not yet fixed.

At step 516, the second cable and third cable may be installed in thewatercraft. As discussed above in connection with method 400, installingthe cables may include routing the cables through a plurality ofwatertight compartments, or through one or more pipes, ducts, cabletrays, cable ladders, retaining rings, watertight cable throughways orpass-throughs or other elements.

At steps 518 and 520 respectively, the cut ends of the second and thirdcables may be terminated. In some embodiments, terminating these endsmay include cutting the second and/or third cable to a final length,removing the safety margin discussed above. In another embodiment, asdiscussed above, terminating the cut ends may include not connecting ashield, braid, or shield drain wire to create a consistent telescopicshield.

B. Electrical Cable Termination and Testing

Various electrical cables may be used with the methods and systemsdiscussed herein. In some embodiments, electrical cables used mayinclude single-conductor cables, such as grounding wires. In otherembodiments, electrical cables used may comprise multi-conductor cables,including coaxial or twinax cables, triaxial cables, ribbon cables,shielded cables, and multi-core cables, including twisted pair,multi-pair, star-quad, and other types of cables. In some embodiments,electrical cables used with the methods herein may include a combinationof one or more cable types, such as coaxial twisted-pair or star-quadhybrid cables. Electrical cables may be used to feed power, controlactuators, provide telemetry or sensor data, for communications, audio,video, or data signals, or for other purposes.

In some embodiments, cable meeting a military standard or “MIL-SPEC”cable may be used. Common types include the MIL-DTL-2463 series and theMIL-DTL-24640 series, although other standards may be used.

Various connectors may be used to terminate cables, and terminations mayinclude crimping, soldering, or a combination of crimping and soldering.Any type or form of connector may be used, from RJ-45 connectors usedfor Ethernet data, to BNC connectors used for video and digital audio,to high-density multi-pin connectors. Connectors may be cable-mount orin-line plugs or receptacles, panel or box-mount plugs or receptacles,or any other type of connector. In some embodiments, MIL-SPEC connectorsmay be used, including the M28840 series, the D38999 series, andMIL-C-5015 series, although other standards may be used.

As discussed above, for safety reasons, it may be undesirable to performsome termination and cable tests after a cable has been installed into awatercraft. Accordingly, installers may only be able to performlow-voltage pin-through continuity checks of installed cables, and maymiss one or more problems with the cable or terminations. However, usingthe methods discussed above, the cable and those terminations performedat the factory may be much more thoroughly tested. In some embodiments,a cable manufacturer may perform one or more tests, including:

Short test—determine if two conductors of a multi-conductor cable arecontacting each other, either in the cable or within a terminated end;

Open test—determine if there's a lack of continuity on a conductor fromone terminated end to the other terminated end;

Mis-wire test—determine if each pin in a termination or connector iscorrectly wired to the corresponding pin or pins in the termination orconnector at the opposite end of the cable;

Low voltage insulation resistance test—determine if the wire insulationhas been damaged or compromised within the terminations or cable;

Connection resistance—determine if resistance within the connector iswithin an acceptable range;

High voltage (hi-pot) test—use a high voltage on one or more conductorsand check for voltage on other conductors to check for dielectricbreakdown or intermittent short circuits;

High strand test—in many embodiments, a wire may be a stranded conductorrather than a solid conductor. During termination, particularly incrimped connections, a strand may be accidentally separated from or“poke out” of the crimp, resulting in a potential short. Because thestrands may be very small in diameter, individual strands may have ahigh resistance and short circuits may not be detected with a lowvoltage test. By using a high voltage, these short circuits may bedetected;

Foreign object debris test—debris in a termination may provide ahigh-resistance path for a potential short circuit that may not bedetected with a low voltage test, or may serve as a conduction path atlow voltage but may burn under high voltage and result in an opencircuit. By using a high voltage, these potential short circuits or opencircuits caused by foreign objects may be detected;

Time-domain reflectivity (TDR) test—measure length to a break in aconductor using a high frequency pulse; and

Impedance test—check impedance of the cable or conductors at one or morefrequencies across a range.

In some embodiments, one or more of these tests may be performed with anautomated cable tester, allowing high speed testing of a large number ofcombinations of conductors in a multi-conductor cable.

C. Optical Cable Termination and Testing

Optical fiber cables or bundles of optical fibers are frequentlyinstalled on watercraft for high-speed data communications. Opticalfibers tend to be more fragile than copper conductors, and may requiremore specialized techniques for termination. For example, while copperconductors are frequently crimped or soldered and a solid mechanicalconnection results in a good electrical connection, optical fibers needto be precisely cut, aligned and polished for transmission of lightwithout loss. Terminating an optical fiber typically includes removinginsulation or an outer sheath at an end section of the fiber; cleaningthe fiber to remove resin and other manufacturing remnants; cleaving theend either flush or with a precise curvature; installing the fiber intoan adhesive filled ferrule; and attaching a connector to the ferrule.

Because the signal transmitted between optical fibers is light,contaminants may block the transmission of the light from or into theend face of the optical fiber. Furthermore, these contaminants mayscratch the end face of the fiber, which may affect the ability of thefiber to transmit a signal, even after the contaminant is removed.Accordingly, during termination, the fiber may be cleaned and polishedto a high degree to reduce optical attenuation.

The above steps may be difficult to perform for installers in crampedlocations on a watercraft under construction or during retrofit orrepair. Stray particles of metal, rust, paint, dust, and othercontaminants could reduce the effectiveness of a field-terminatedconnection or cause it to fail completely. By terminating one end of acable in a factory, clean room standards can be used and automatedpreparation, cutting, termination, cleaning and polishing machines maybe employed. This may drastically reduce failure rates of opticalcables. Furthermore, because only one end of the cable will befield-terminated and is thus significantly more likely to fail than theopposite end, if the cable fails to perform adequately, troubleshootingcan be cut nearly in half by examining the field-terminated end first.

In some embodiments, MIL-SPEC optical fiber cables may be used, such asthe M85045 series specification of cables. Similarly, MIL-SPECconnectors may be employed, such as the M28876 or MIL-ST (also referredto as M83522) series connectors. In other embodiments, other standardsor grades of optical fiber or connectors may be used, including hybridoptical-electrical cables and connectors.

In some embodiments, terminated optical cables may be tested for loss bysending a known amount of light through one terminated end of the fiber,and measuring the amount of light exiting the opposing end. In furtherembodiments, loss may be determined at one or more wavelengths of light,which may be important particularly for wavelength-division multiplexingfor higher data rates. In other embodiments, an optical time domainreflectometer (OTDR) may be employed to measure the length of a fiber orthe length to a break, or to measure back reflection or optical returnloss. In still other embodiments, optical fibers may be tested fordispersion, optical bandwidth, or other features.

CONCLUSION

Although discussed above in terms of new construction and outfitting ofa watercraft, the methods and systems described herein may be readilyapplied by one of skill in the art to retrofitting, refurbishing,repair, or upgrading of systems in previously constructed and/oroutfitted watercraft.

While various embodiments of the methods and systems have beendescribed, these embodiments are exemplary and in no way limit the scopeof the described methods or systems. Those having skill in the relevantart can effect changes to form and details of the described methods andsystems without departing from the broadest scope of the describedmethods and systems. Thus, the scope of the methods and systemsdescribed herein should not be limited by any of the exemplaryembodiments and should be defined in accordance with the accompanyingclaims and their equivalents.

What is claimed is:
 1. A method, comprising: providing a cable;attaching a termination at a first end of the cable at a locationdifferent from a watercraft; and supplying the cable unconnected ateither end for installation onto the watercraft with the terminationattached at the first unconnected end of the cable and a secondunconnected end of the cable being non-terminated such that thenon-terminated second end is routable through a throughway on thewatercraft, wherein the cable is configured for installation on thewatercraft to connect and provide a communication path between aplurality of components of the watercraft.
 2. The method of claim 1,further comprising testing the cable prior to supplying the cable forinstallation onto the watercraft.
 3. The method of claim 1, furthercomprising: installing the cable onto the watercraft through thethroughway; and installing a termination onto the second end of theinstalled cable.
 4. The method of claim 3, wherein the throughway is amulti-cable throughway in a watertight bulkhead of the watercraft. 5.The method of claim 3, wherein the installing the cable onto thewatercraft includes routing the cable through a plurality of watertightcompartments.
 6. The method of claim 1, wherein the cable is an opticalfiber cable.
 7. The method of claim 2, wherein the testing of the cableincludes sending a known amount of light through the first end of thecable or the second end of the cable, the light traveling via opticalfibers of the cable.
 8. The method of claim 7, wherein the testing ofthe cable further includes measuring an amount of light exiting the endof the cable opposite the end through which the known amount of light issent.
 9. The method of claim 2, wherein the testing of the cableincludes performing a measurement via an optical time domainreflectometer.
 10. The method of claim 1, further comprising: prior tosupplying the cable for installation onto the watercraft, attaching atermination to a second end of the watercraft; after attaching thetermination to the second end of the cable and prior to supplying thecable for installation onto the watercraft, testing the cable; and aftertesting the cable, removing the termination from the second end of thecable.
 11. The method of claim 1, further comprising: forming the cableby cutting a length of cable that is longer than the cable; and prior toforming the cable, testing the length of cable that is longer than thecable.
 12. A method for installation of cable into a watercraft, themethod comprising: providing a cable with a first end and a second end;at a location different from a watercraft, installing a termination atthe first end of the cable and a termination at the second end of thecable; cutting the cable at a location between the first and second endsto form first and second cable sections each having a terminated firstend and a non-terminated second end; and supplying at least the firstcable section having the terminated first end and the non-terminatedsecond end for installation onto the watercraft, wherein the cable isconfigured for installation on the watercraft to connect and provide acommunication path between a plurality of components of the watercraft,the at least the first cable section being supplied with the terminatedfirst end unconnected and the non-terminated second end unconnected. 13.The method of claim 12, further comprising: installing the first cablesection onto the watercraft; and installing a termination onto thesecond end of the installed first cable section at the watercraft. 14.The method of claim 12, further comprising: providing the second cablesection, having the terminated first end and the non-terminated secondend, for installation onto the watercraft.
 15. The method of claim 14,further comprising: installing the first cable section onto thewatercraft; and installing a termination onto the second end of theinstalled second cable section at the watercraft.